Mh-53e Helicopter Parts

(Page 167) End item NSN parts page 167 of 238
Part Number
NSN
NIIN
11205-05 Tapered Roller Bearing
006908923
11205-094 Composition Fixed Resistor
002521050
11207483-3 Electrical Contact
010990068
1120B SOLDER Stud Terminal
000824890
1121-0330 Electric Soldering Iron Tip
013831859
1121-0330-P1 Electric Soldering Iron Tip
013831859
1121-4 Electrical Contact
003389875
1122990 Preformed Hose
003586107
1123-124ITEM3 Plain Encased Seal
005850582
11231P11 Incandescent Lamp
006430687
112386-041 Film Fixed Resistor
011866796
11240444-1 Tube To Hose Straight Adapter
004978280
11240444-4 Tube To Hose Straight Adapter
005882614
11240487-41 Tube Tee
002636480
11241344-1 Standoff Insulator
001421840
11252 Headed Straight Pin
008111232
11253024-3 Ceramic Dielectr Fixed Capacitor
000642919
1126010-8 Turnlock Fastener Stud Assembly
006395575
11269318 Plate Self-locking Nut
005848164
112697R1 S Chain Hook
002705436
Page: 167 ...

Helicopter, Mh-53e

Picture of Mh-53e Helicopter

The Sikorsky CH-53E Super Stallion is the largest and heaviest helicopter in the United States military. As the Sikorsky S-80 it was developed from the CH-53 Sea Stallion, mainly by adding a third engine, adding a seventh blade to the main rotor and canting the tail rotor 20 degrees. It was built by Sikorsky Aircraft for the United States Marine Corps. The less common MH-53E Sea Dragon fills the United States Navy's need for long range minesweeping or Airborne Mine Countermeasures (AMCM) missions, and perform heavy-lift duties for the Navy. Under development is the CH-53K King Stallion, which will be equipped with new engines, new composite material rotor blades, and a wider aircraft cabin.

The CH-53 was the product of the U.S. Marines' "Heavy Helicopter Experimental" (HH(X)) competition begun in 1962. Sikorsky's S-65 was selected over Boeing Vertol's modified CH-47 Chinook version. The prototype YCH-53A first flew on 14 October 1964. The first CH-53As were powered by two General Electric T64-GE-6 turboshaft engines with 2,850 shp (2,125 kW) and had a maximum gross weight of 46,000 lb (20,865 kg) including 20,000 lb (9,072 kg) in payload.

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